N325QS, cancelled Jun 9, 2011
Service difficulty reports · 20
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N325QS' AND deregistration_id = 'N325QS-2011-06-09' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N325QS' AND deregistration_id = 'N325QS-2011-06-09' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DXTA2010080904188Brake Sys · weakBRAKES SPONGY BOTH PEDALS, BOTH SIDES. BLEED LT AND RT BRAKE SYS IAW MM 32-40-00. OPS CHECKED SATISFACTORY.SDR DXTA200807183181Starter Gen · faultyLT FUEL FLOW FLUCTUATION DURING CLIMB AND CRUISE FOLLOWED BY LT GEN FAILURE, FOLLOWED BY LT ENGINE VIBRATION SUB: FOUND LT START GEN EXHAUST DUCT HAS LARGE AMOUNT OF SOOT. REMOVED AND REPLACED LT START GEN. C/W SATISFACTORY, OPS CHECK AND PARALLEL IAW MM 24-SDR DXTA200803181Fuel Sys · fluctuatesLT FUEL FLOW FLUCTUATION DURING CLIMB AND CRUISE FOLLOWED BY LT ENG FAILURE, FOLLOWED BY LT ENGINE VIBRATION.SDR DXTA200803141Control Cable · out of rigTHE AIRCRAFT HAS AN AGGRESSIVE ROLL LEFT WITH THE ASSOCIATED TRIM TAB CENTERED. PLACED A YOKE LEVEL ON THE YOKES AND OPENED THE AFT CABIN FLOOR. INSERTED A RIG PIN IN THE AILERON SECTOR. PLACED THE AILERON TRIM TO NEUTRAL. FOUND THE RT AILERON ABOVE STREAM LISDR DXTA200702324Vertical Gyro · faultyAUTOPILOT MALFUNCTION - LEVEL AT 41000 MSL, THE AUTOPILOT AGGRESSIVELY PITCHED UP TO OVER 1000 FPM. THE AUTOPILOT WAS DISCONNECTED. AFTER 1 MINUTE, THE AUTOPILOT WAS RECONNECTED AND PROBLEM REOCURRED. REMOVED FAULTY LT SIDE PITOT STATIC PORT HOSE AND NR 1 SDR DXTA200702104Unknown · unknownDESCENDING THROUGH 11,000 FT, RT ENGINE LOW FUEL PRESSURE ANNUNCIATOR ILLUMINATED, TRIGGERING RT FUEL BOOST ANNUNCIATOR TO ILLUMINATE. RAN THE ABNORMAL CHECKLIST AND LANDED. NO ENGINE FLUCTUATIONS OR OTHER ENGINE INDICATIONS WERE NOTED. [SUP 4-19-07] SUMPSDR DXTA200702004Master Cylinder · malfunctionedLT BRAKE ON RT SIDE TRAVELS ALMOST TO FLOOR DURING BRAKE APPLICATIONS. REMOVED CO-PILOTS IB AND OB BRAKE MASTER CYLINDERS AND INSTALLED NEW MASTER CYLINDERS IAW C560 MM 32-42-02. BLED BRAKES AS REQUIRED.SDR DXTA200701848Coalescer Bag · dirtySHARP IRRITATING ODOR/SMELL MAINLY IN COCKPIT, STRONGER RIGHT AFTER TAKE OFF REMAINED THROUGH WHOLE FLIGHT INCREASED AGAIN DURING DESCENT. RAN ENGINES FOR 30 MINUTES AT 70% FOUND NO ODOR. CHECK OIL LEVELS GOOD. NO SIGN OF EXTERNAL OIL LEAKS. CHECK ACM OIL LEVESDR DXTA200601679Brake · malfunctionedRIGHT SEAT LEFT BRAKE REQUIRES MORE PRESSURE FOR RESPONSIVENESS COMPAIRED TO RIGHT SEAT RIGHT BRAKE. SERVICED AND BLED BRAKE SYSTEM IAW CESSNA 560 MM CH. 32-42-00SDR DXTA200601644Hose · kinkedDURING TAXI WHEN MAKING A SHARP LEFT TURN, FULL DEFLECTION OF RUDDER PEDALS, F/O'S LEFT BRAKE PEDAL WOULD BECOME STIFF AND ROLL FORWARD, UPON STRAIGHTENING NOSE GEAR BRAKES RETURNED TO NORMAL, ONLY ON F/O SIDE, ONLY DURING LEFT TURN. M2B - T/S TO LOWER HOSE OSDR DXTA200601631Brake Assy · malfunctionedWHEN LEFT RUDDER PEDAL IS PUSHED TO THE FLOOR AND THEN LT BRAKE IS APPLIED THERE IS NO PRESSURE AND TRAVELED TO THE FLOOR WITH NO BRAKING ACTION. BLED BRAKES AS PER CE560 AMM 32-42-00. BRAKE SYSTEM OPERATED NORMALLY DURING NORMAL BRAKING, AND WITH FULL RUDDERSDR DXTA200601578Brake · leakingDURING TAXI AIRCRAFT PULLS HARD TO RIGHT WHEN BRAKES ARE APPLIED; POST FLIGHT INSPECTION SHOWS SMALL FLUID LEAK ON FRONT SIDE OF LEFT BRAKE.SDR DXTA200601471Brake · contaminatedBRAKES VERY SOFT, YOU HAVE TO PUSH BRAKE PEDALS A LOT FURTHER THAN NORMAL TO MAKE BRAKES WORK IAW CESSNA 560 MM 32-42-00, PERFORMED BRAKE BLEEDING MAINTENANCE PROCEDURE. FOUND LARGE AMOUNTS OF AIR IN SYSTEM ALONG W/ LOW BRAKE FLUID LEVEL. REMOVED AIR AND REPSDR DXTA200501139Fcu · failedDID NOT GET FULL PWR ON RIGHT HAND ENGINE DURING STATIC TAKEOFF, N1 75.9 ITT 450, N2 83 WITH THROTTLES FULL FWD. REMOVED AND REPLACED RIGHT ENGINE FCU AND FUEL PUMP. ENGINE OPERATES NORMAL AT THIS TIME IAW PWA M/M 71-00-00.SDR DXTA200501045Brake · malfunctionedPILOTS LEFT BRAKE ALMOST GOES TO THE FLOOR. ITEM IS UNDER INVESTIGATION.SDR DXTA200501041Transducer · malfunctionedCAPT LEFT BRAKE PEDAL INTERMITTENTLY LOSES PRESSURE IN TURNS. REMOVED AND REPLACED LT ANTI SKID TRANSDUCER IAW CE 560 MM 32-42-07.SDR DXTA200501021Brake Assy · weakCOPILOT'S BRAKE PEDALS ARE SOFT. ITEM IS UNDER INVESTIGATION.SDR 20001205SH007Skin · corrodedUPON INSPECTION OF WING DEICE BOOTS, THE AERODYNAMIC FILLER WAS DETERMINED TO BE SEPARATING FROM SKIN CAUSING THE DEICE BOOT TO DEBOND. THE DEICE BOOT WAS REMOVED AND SKIN CLEANED OF DEFECTION FILLER. AT THIS TIME, THE SKIN WAS FOUND TO BE CORRODED AT THE LOSDR 20001205SH006Skin · corrodedUPON INSPECTION OF WING DEICE BOOTS, THE AERODYNAMIC FILLER WAS DETERMINED TO BE SEPARATING FROM SKIN CAUSING THE DEICE BOOT TO DEBOND. THE DEICE BOOT WAS REMOVED AND SKIN CLEANED OF DEFECTION FILLER. AT THIS TIME, THE SKIN WAS FOUND TO BE CORRODED AT THE LOSDR 99ZZZX11Nut · missingWHILE INSPECTING LANDING GEAR ASSY DETERMINED BOTH MAIN LANDING GEAR SQUAT SWITCHES MISSING JAM NUT THAT SECURES THE ROD END TO THE TORQUE LINK. THE SQUAT SWITCH ASSY COULD BE TURNED AND MOVED.
Back to N325QS, cancelled Jun 9, 2011